Deployable Techniques for Small Satellites

Miyazaki, Yuji

doi:10.1109/jproc.2018.2799608

Cited by 30 publications

(14 citation statements)

References 39 publications

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“…Satellites (Sweeting, 2018), (Miyazaki, 2018), (Nambu et al, 2019), (Bedington et al, 2016), (Parco et al, 2013), (Herrera Arroyave et al, 2015), (Burgos González, 2016), (Mozombite Frisancho, 2012), (Islam et al, 2019), (Ramadhan et al, 2019) Measurement (Pető, 2013), (Bulut et al, 2013), (Colin, 2015), , (Mendieta Daza et al, 2017), (Buitrago et al, 2019) Design (Kizilkaya et al, 2017), (Colín et al, 2016), (González-Llorente et al, 2012), (Santiago Flores et al, 2016), (Mancilla Cerezo et al, 2019), (Mafra de Carvalho et al, 2013), Testing (Ostaszewski Michałand Dzierzek & Magnuszewski, 2018), (Colin, 2016), (Krejci & Lozano, 2018), (Friend et al, 2016), (Hernandez, 2012), (Mendoza et al, 2015) Applications (Çabuloglu et al, 2011), (Lee et al, 2017), , (Anchino et al, 2019) Martino, 2013), (Pablo et al, 2014) Others (Davoli et al, 2019), (Madry et al, 2018) A characteristic that cannot be omit-ted to carry out the review of small satellites is the year of publication of the documents, with the purpose of differentiating the increasing research in this field. Therefore, the documents were discriminated by year of publication, in order to differentiate the largest number of documents in the last 5 years.…”

Section: Reference Documentsmentioning

confidence: 99%

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A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world

Soto

Figueredo

Cañón³

et al. 2020

GRAINE

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Small satellites have been a fundamental factor in the constant growth of space technologies from 60 years ago. Since the space war began during the Cold War, thousands of satellites have been put into low orbit to carry out radio frequency applications, analysis and sending satellite images of the earth, joint research tasks for space exploration on artificial satellites, as well as missions in other astronomical bodies. By 2019, more than 50 countries around the world have put into orbit at least 1 small satellite, which accounts for the persistent work to increase the applications of these devices and the need make known the potential of these elements for research and for technological applications. Due to this, the present article was based on the documentary search to carry out a review of the current state of small satellites, and especially of nano and pico satellites. The research defined 3 phases for the writing of this document: choice of databases and search engines according to the research area, use of selection algorithms using logical discrimination chains and, finally, extensive analysis of the chosen documents for the writing of the article. All the information was presented through statistical graphs with detailed information from years of publication, language, region, terms, and areas the greatest research of small satellites. It was found that CubeSat and CanSat are the types of nano and pico satellite with the greatest predilection for research by universities and technological institutions, given its low cost and in most cases its easy implementation.

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Section: Reference Documentsmentioning

confidence: 99%

“…In addition to the above, it is necessary to add some contributions that are presented for the structural design and commissioning of these satellites. On the one hand, the authors in (Miyazaki, 2018) mention some deployment structures in orbit for small satellites, addressing the most widely used, among which are:…”

Section: Outside Latin America Contributionsmentioning

confidence: 99%

A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world

Soto

Figueredo

Cañón³

et al. 2020

GRAINE

View full text Add to dashboard Cite

show abstract

“…Here ∆Φ Q is the discrete quantized phase shift introduced by a unit cell, ∆Φ C is the desired continuous phase from that particular unit cell as calculated using (1), and % represents the modulo (remainder) operator. In our variable length implementation to produce the required phase shift from a unit cell, a corresponding set of 8 lengths was selected using (9) to (11).…”

Section: Phase Quantized Reflectarray Designmentioning

confidence: 99%

“…To allow further compactness, reflectarrays can be folded into a compact form during launch, and then can be unfolded and deployed once in orbit. To further facilitate the compactness, reflectarrays can be made inflatable [8][9][10]. A reflectarray can implement any reflector antenna configurations to fit the requirements.…”

Section: Introductionmentioning

confidence: 99%

An investigation of millimeter wave reflectarrays for small satellite platforms

et al. 2018

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“…A deployable structural system for space application must be simple, lightweight, and able to withstand the high loading condition during the launching phase while assuring low cost (Miyazaki, 2018). Deployable structures also need their own deployment mechanisms to change from the stowed state to the operational state.…”

Section: Introductionmentioning

confidence: 99%

A two-dimensional modular deployable truss structure with bistability

Suh

Jeong

Han

2018

Journal of Intelligent Material Systems and Structures

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In this article, a new concept of two-dimensional modular deployable truss structure is proposed. To eliminate additional needs of containment mechanism, the proposed deployable structure is designed to have bistable characteristics so that it can stay robust both in the stowed and deployed states. The deployment of each module is triggered by the actuation of shape memory alloys. Static and dynamic models of the proposed deployable structure are established to analyze the characteristics and behavior of the system. The packaging ratio of the proposed structure is analyzed in terms of the design parameters. The results of static and packaging efficiency analysis show that the proposed concept has operational flexibility and high packaging efficiency. Verification of the dynamic model is performed based on a comparison of the response of the dynamic model and the actual deployment process of an experimental model; the deployment process is captured using a stereo pattern recognition camera system. It is shown that the established dynamic model can accurately describe the deployment behavior of the proposed structure.

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Deployable Techniques for Small Satellites

Cited by 30 publications

References 39 publications

A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world

A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world

An investigation of millimeter wave reflectarrays for small satellite platforms

A two-dimensional modular deployable truss structure with bistability

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